Investigation of thrusters for cryogenic reaction control systems, volume 1 Final report, Jun. 1968 - Oct. 1969
Ignition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrusters at cryogenic temperatures
SEARCH · Engineering Papers
Search indexed NASA NTRS and DOE OSTI research on propulsion, heat transfer, battery materials and energy systems. Follow report and document links to the original sources.
Quote a phrase for an exact phrase match. Source license links do not imply unrestricted reuse.
Ignition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrusters at cryogenic temperatures
Ignition characteristics and delivered performance of gaseous hydrogen-oxygen reaction control thrusters at cryogenic temperatures - appendices
Effects of backsputtered material on performance of glass coated accelerator grids for electron bombardment thrusters
Characteristics of SERT thruster with argon propellant
Plasma measurements in SERT 2 spacecraft ion thruster discharge chamber using Langmuir probe
Effects of mercury electron bombardment ion thruster exhaust products on surfaces located downstream
Thruster exhaust effects on spacecraft structures
Electron bombardment hollow cathode ion thruster performance
Operational performance of electron bombardment mercury ion thruster system during life testing in space simulation for SERT 2
Theoretical analysis of performance of two-grid accelerator systems for Kaufman thrusters
Flow equation for representing ion beam current density profile from bombardment ion thrusters
Research in optimization of performance, and performance characteristics of annular slit colloid thruster
Prototype auxiliary propulsion subsystem with isolated single tank propellant feed system and 5-cm-diameter ion thruster
Research and development of mercury electron bombardment thrusters
Development and tests of flight prototype power conditioner for 20 cm mercury bombardment electric thruster system
Development and characteristics of ion thruster accelerator with single glass coated grid to provide increased ion extraction capability and larger diameter accelerator system
System for removing and repairing spacecraft control thrusters by use of portable air locks
Fabrication and testing of bonded metal-ceramic, glass-coated metal, and glass-coated ceramic bonded to metal composite electrodes for cesium bombardment ion thrusters